PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM LABEL_REVISION_NOTE = "20200206 R. Lorenz and L. Huber" OBJECT = MISSION MISSION_NAME = {"VEGA 1", "VEGA 2"} OBJECT = MISSION_INFORMATION MISSION_START_DATE = 1984-12-15 MISSION_STOP_DATE = 1986-04 MISSION_ALIAS_NAME = "N/A" MISSION_DESC = " Mission Overview ================ The return of Halley's comet in 1985/86 provided a unique opportunity to combine a mission to explore Venus, (continuing the Venera lander series) with exploration of Halley by employing a two-element space vehicle comprising a Venus lander (and balloon) and a carrier spacecraft which would go on to Halley. The mission was called VeGa, a contraction of the Russian words 'Venera' (Venus) and 'Gallei' (Halley) and was conducted by the USSR with scientific payloads and ground tracking support from several countries, notably France and the USA. The Project Scientist was Roald Z. Sagdeev of the Institute for Space Research (IKI) in Moscow. Like many Soviet planetary missions, Vega comprised two identical spacecraft, Vega 1 and Vega 2. This was a standard Soviet approach to ensure the overall reliability of the mission. If both spacecraft were successful there would be a significant increase in the scientific return, which was particularly valuable in the case of the Halley flybys given the variability of comet activity. The two spacecraft were launched by Proton rockets from the Baikonur cosmodrome on 15 and 21 December 1984, respectively. On 11 and 15 June 1985, the two spacecraft successfully delivered lander entry vehicles into the Venus atmosphere. During the descent of these landers, each released a helium-filled balloon to float near the cloud tops. The landers each reached and survived on the surface for about an hour, while the balloons operated for about 2 days. The Vega 1 and Vega 2 'mother' spacecraft went on to encounter comet Halley on 6 and 9 March 1986, respectively. During early planning of the mission, larger French-led balloons had been considered but the inclusion of comet Halley in the mission plan for the flyby spacecraft forced the use of the smaller, Soviet balloons eventually flown. Both balloons were successful, transmitting for 46.5hrs in the nightside atmosphere while being tracked by an international network of radio telescopes on Earth which received the data directly from the balloons on a very low data-rate one-way radio link (4 bits per second transmitted initially for 270 s every 30 minutes 4.5W at 1.667 GHz). The balloons were small (3.54m diameter) and filled with ~2kg of helium from tanks carried on the landers. The balloon scientific return was ultimately limited by energy, supplied by lithium primary batteries (~1 kg, 250 W-hr). Their payload was austere (the whole gondola was 6.9kg), with pressure and temperature sensors, a light level/lightning detector, a nephelometer (cloud backscatter sensor) and a lightweight 'windmill' vertical anemometer. Additional investigations included Doppler measurements to retrieve turbulence and windspeed, and position measurements using the Differential Very Long Baseline Interferometry (DVLBI) technique. The spherical entry vehicles were ~1750kg in mass, including entry thermal protection extraction parachutes, and the helium tanks for the balloons. The landers themselves were ~750kg and took about 1 hour to reach the surface. The landers carried a variety of instrumentation for study of the atmosphere and surface. " MISSION_OBJECTIVES_SUMMARY = "See SAGDEEV1986H and SAGDEEV1986I." END_OBJECT = MISSION_INFORMATION OBJECT = MISSION_HOST INSTRUMENT_HOST_ID = {"VEGA1", "VEGA2"} OBJECT = MISSION_TARGET TARGET_NAME = VENUS END_OBJECT = MISSION_TARGET END_OBJECT = MISSION_HOST OBJECT = MISSION_REFERENCE_INFORMATION REFERENCE_KEY_ID = "KREMNEV1986" END_OBJECT = MISSION_REFERENCE_INFORMATION OBJECT = MISSION_REFERENCE_INFORMATION REFERENCE_KEY_ID = "SAGDEEV1986H" END_OBJECT = MISSION_REFERENCE_INFORMATION OBJECT = MISSION_REFERENCE_INFORMATION REFERENCE_KEY_ID = "SAGDEEV1986I" END_OBJECT = MISSION_REFERENCE_INFORMATION END_OBJECT = MISSION END